| 000 | 00772pam a2200217a 44500 | ||
|---|---|---|---|
| 005 | 20200612164039.0 | ||
| 008 | 200612b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 082 |
_aNASA _bTN D-1397 |
||
| 100 | _aSpencer,Bernard | ||
| 245 | 1 |
_aLow-speed longitudinal chracteristics of an airplane configuration including effects of canard and wing trailing-edge flap controls in combination[NASA TN D-1397] _cSpencer,Bernard |
|
| 260 |
_bWashington, D.C. _c1962 |
||
| 300 | _a47p | ||
| 440 | _aNational aeronautics and space administration (NASA) | ||
| 500 | _aBound With Nasa Tn D-1391-1396,1398-1400. | ||
| 505 | _aNASA technical report | ||
| 650 | _aLow-speed | ||
| 700 | _aBernard Spencer and William C. Sleeman | ||
| 942 | _cREF | ||
| 999 |
_c399123 _d399123 |
||